Airplane Flight Manual Supplement

AFMS, GARMIN G500/G600 SYSTEM 190-00601-01 Rev. K
FAA APPROVED Page 17 of 51
1.12 Single G500/G600 Operational Block Diagram
Standby
Attitude*
Standby
Airspeed
Standby
Altimeter
Magnetic
Compass
Equipment Installed per this STC
(required)
PFD/MFD Display
GDU 620
*Standby Attitude: may be replaced
with electric attitude indicator with
integral / dedicated backup battery.
**Audio panel connection to GDU 620
is recommended for tones and aural
alerts generated by the GDU 620.
This MUST be connected if TAWS
and/or SVT is enabled.
*** Installation of the Mid-Continent
electric standby attitude indicator is
approved by this STC.
Air Data Computer
AHRS
Magnetometer
GMU 44
GRS 77
GDC 74()
Temperature Probe
GTP 59
No. 1 GPS/SBAS Navigator
(required)
No. 1 VOR/Localizer/GS
(optional)
No. 2 GPS/SBAS Navigator
(optional)
No. 2 VOR/Localizer/GS
(optional)
Autopilot/Flight Director
(optional)
ADF, DME
(optional)
Audio Panel
(optional)**
Traffic
(optional)
Datalinks
(optional)
Adapter (optional)
GAD 43/43e
Aircraft Systems
Weather Radar
(optional)
Electric
Standby
Attitude***
(optional)
Radar Altimeter
(optional)
Stormscope
(optional)
Existing Equipment
(already installed in aircraft)
Video Source
(optional)